What was found
SVC - FLT 31J - INSPECTION FOUND A 10 INCH CRACK IN FUSELAGE SKIN AT BS 449 TO 469 STR 16R. THE CRACKED SECTION WAS REMOVED, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-03. (Z)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
SVC - FLT 31J - INSPECTION FOUND A 10 INCH CRACK IN FUSELAGE SKIN AT BS 449 TO 469 STR 16R. THE CRACKED SECTION WAS REMOVED, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-03. (Z)